Bubble Wing
DOI:
https://doi.org/10.32628/IJSRSET251213Keywords:
Bubble Wing, Compression, ExpansionAbstract
This study explores modifications to airfoil structures designed to reduce aircraft speed during critical situations, enabling smoother and safer emergency landings. By optimizing aerodynamic performance, the proposed design minimizes impact forces upon ground contact. The results provide a foundation for integrating advanced airfoil designs into emergency response protocols.
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Mariza D. Ardany, Paken Pandiangan and Moh. Hasan (2021), “Lift Force of Airfoil (NACA 0012, NACA 4612, NACA 6612) With Variation of Angle of Attack and Camber: Computational Fluid Dynamics Study” Computational and Experimental Research in Materials and Renewable Energy (CERiMRE) Volume 4, Issue 2, page 80-93 eISSN : 2747-173X DOI: https://doi.org/10.19184/cerimre.v4i2.28372
Antony Jameson and James Rethuer, (1988) “Control Theory based airfoil design using Euler's equations". DOI: https://doi.org/10.1007/BF01061285 DOI: https://doi.org/10.1007/BF01061285
T Gultop, (1995) “An Investigation of the effect of aspect ratio on Airfoil performance.” American Journal of Applied Sciences ISSN/EISSN: 15469239 15543641, Volume: 2, Issue: 2, Pages: 545-549. DOI: https://doi.org/10.3844/ajassp.2005.545.549
J. Fazil and V. Jayakumar, (2011) “INVESTIGATION OF AIRFOIL PROFILE DESIGN USING REVERSE ENGINEERING BEZIER CURVE”, Journal: Journal of Engineering and Applied Sciences ISSN 1819-6608 Volume: 6; Issue: 7
M Afzaal Malik, Farooq Ahmad (2010),” Effect of Different Design Parameters On Lift, Thrust and Drag of an Ornithopter” Proceedings of the World Congress on Engineering 2010 Vol II WCE 2010, June 30 - July 2, 2010, London, U.K.
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